Guidance and trajectory for a missile
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Trajectory and guidance analysis
this question is from advance weapon system about flying a proectile
You are to evaluate guidance laws while flying a projectile to a stationary intercept point in your 2-D simulation (use the ProjectileFramework Matlab script). You will evaluate how the initial conditions of a guidance law effect the trajectory shape, and you are to prove (or disprove) basic guidance optimization criteria, and common “rules of thumb” in the guidance field
![](https://www.mathworks.com/matlabcentral/answers/uploaded_files/289339/image.jpeg)
![](https://www.mathworks.com/matlabcentral/answers/uploaded_files/289340/image.jpeg)
2 件のコメント
Image Analyst
2020 年 5 月 1 日
For what it's worth, attached is my demo for computing and showing just about everything you could possibly want to know about trajectory and a projectile. It has variables/parameters for initial conditions like height, speed, angle, etc.
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